General Aviation Aircraft/Fuel System Configuration Study Regarding Fuel Bladder Cell Installation

871011

05/01/1987

Event
General Aviation Aircraft Meeting and Exposition
Authors Abstract
Content
The general aviation community, acting through an informal organization known as the General Aviation Safety Panel (GASP), has sought to develop meaningful recommendations in the area of crashworthiness as it applies to post-crash fires. In support of the GASP efforts the potential fuel volume reduction and weight penalties that might be incurred should crash resistant fuel systems be installed in general aviation fixed-wing aircraft were quantified. A wide range of aircraft sizes and configurations were evaluated and relationships were developed between various aircraft/fuel system parameters to estimate the potential impact that installation of fuel bladder cells might have on aircraft design.
Meta TagsDetails
DOI
https://doi.org/10.4271/871011
Pages
8
Citation
Soltis, S., "General Aviation Aircraft/Fuel System Configuration Study Regarding Fuel Bladder Cell Installation," SAE Technical Paper 871011, 1987, https://doi.org/10.4271/871011.
Additional Details
Publisher
Published
May 1, 1987
Product Code
871011
Content Type
Technical Paper
Language
English